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Volumn 426, Issue , 2001, Pages 73-94

Leading-edge receptivity of a hypersonic boundary layer on a flat plate

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVES; PERTURBATION TECHNIQUES; PLATES (STRUCTURAL COMPONENTS);

EID: 0035835272     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112000002147     Document Type: Article
Times cited : (157)

References (35)
  • 12
    • 0016483071 scopus 로고
    • Wind tunnel experiments relating to supersonic and hypersonic boundary-layer transition
    • (1975) AIAA J , vol.13 , pp. 290-299
    • Kendall, J.M.1
  • 20
    • 33748717393 scopus 로고
    • Some statistical properties of the pressure field radiated by a turbulent boundary layer
    • (1964) Phys. Fluids , vol.8 , pp. 1191-1197
    • Laufer, J.1
  • 22
    • 0016483098 scopus 로고
    • Linear stability theory and the problem of supersonic boundary layer transition
    • (1975) AIAA. J , vol.13 , pp. 423-448
    • Mack, L.M.1
  • 29
    • 0010980249 scopus 로고
    • The use of Pitot tubes in the measurements of laminar boundary layers in supersonic flow
    • (1957) ARC R. and M , pp. 3056
    • Monaghan, R.J.1
  • 30
    • 0004042201 scopus 로고
    • Critical evaluation of transition from laminar to turbulent shear layers with emphasis on hypersonically travelling bodies
    • (1969) AFFDL-TR 68-149
    • Morkovin, M.V.1
  • 32
  • 35
    • 2942734338 scopus 로고    scopus 로고
    • Direct numerical simulation of hypersonic boundary layer transition over blunt leading edges, part 2: Receptivity to sound
    • (1997) AIAA Paper 97-0756
    • Zhong, X.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.